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Multi-Objective Optimization of a Diodic ProfileThe present paper investigates the flow physics of Tesla valves and studies how various geometric parameters affect their performance. The performance of the valve is measured by its diodicity, evaluated by comparing pressure drops and discharge coefficients in the forward and reverse flow directions. First, only the flow return angle of a baseline geometry was varied to understand the impact of return angle on valve performance. These baseline geometries are first analyzed with CFD, and then fabricated and installed in a steady-state experimental test rig equipped with pressure transducers, to measure forward and reverse discharge coefficients. Seven additional geometries are also tested in cold flow to identify the impact of diode count, diode volume, and orifice size on valve performance. Next, a multi-objective optimizer is allowed to vary 12 geometric parameters to produce an optimum geometry.
Document ID
20230017999
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
Avidh Bavkar
(Purdue University West Lafayette West Lafayette, United States)
Peter Salek
(Purdue University West Lafayette West Lafayette, United States)
Venkat Athmanathan ORCID
(Purdue University West Lafayette West Lafayette, United States)
Guillermo Paniagua
(Purdue University West Lafayette West Lafayette, United States)
Terrence Meyer ORCID
(Purdue University West Lafayette West Lafayette, United States)
James Braun
(North Carolina State University Raleigh, United States)
Hugh D Perkins
(Glenn Research Center Cleveland, United States)
Chris Fugger
(Spectral Energies LLC Beavercreek, OH, USA)
Date Acquired
December 8, 2023
Subject Category
Spacecraft Propulsion and Power
Meeting Information
Meeting: AIAA SciTech Forum and Exposition
Location: Orlando, FL
Country: US
Start Date: January 8, 2024
End Date: January 12, 2024
Sponsors: American Institute of Aeronautics and Astronautics, Lockheed Martin (United States)
Funding Number(s)
WBS: 264925.04.22.22
CONTRACT_GRANT: 80NSSC22PB194
CONTRACT_GRANT: 80NSSC23CA152
Distribution Limits
Public
Copyright
Public Use Permitted.
Technical Review
Single Expert
Keywords
Propulsion
Detonation
Diagnostics
Fluid Dynamics
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